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04-BS-6 · December 2013

Question 8 of 8: Stepped Shaft in Torsion

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

National Exams December 2013 – 04-BS-6: Mechanics of Materials
3 hours duration, closed book (one hand-written aid sheet permitted). Any five of the eight questions constitute a complete paper; all eight are solved below as a complete study resource.

Reference texts: R.C. Hibbeler, Mechanics of Materials, 10th ed. (Ch. 5 torsion, Ch. 6 shear/moment diagrams & composite beams, Ch. 7 transverse shear, Ch. 8 combined loadings, Ch. 9 stress transformation, Ch. 12 deflection by integration, Ch. 13 buckling); F. Beer & E.R. Johnston, Mechanics of Materials; W. Gere & B. Goodno, Mechanics of Materials (alternates). A W-shape properties table printed on the exam's last page is not needed — every question supplies its own section dimensions.

Question 8: Stepped Shaft in Torsion (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

ABCDE100mm500mm60mm300mm120mm400mm120mm800mmT_A=25 kN·mT_B=30 kN·mT_C=35 kN·mFig. Q8 – stepped shaft in torsion
Stepped aluminum shaft, fixed at E; torques at A (25 CW), B (30 CCW), C (35 CW) kN·m.

Given.

SegmentLength (mm)Diameter (mm)
AB500100 (solid)
BC30060 (solid)
CD400120 (solid)
DE800120 OD / 60 ID (hollow)

G = 25 GPa; TA=25 kN·m (CW), TB=30 kN·m (CCW), TC=35 kN·m (CW); shaft fixed at E.

Find. (a) Maximum shear stress and its radial variation. (b) Angle of twist of A relative to the fixed end E. (c) The effect of doubling all three torques.

Approach. Take clockwise as positive; find the internal torque in each of the four segments by summing the applied torques to the free (A) side of each cut, then apply $\tau=Tr/J$ and $\phi=TL/(GJ)$ segment by segment, summing the angles algebraically.

  1. Internal torque in each segment (CW+). $$T_{AB}=T_A=+25, \quad T_{BC}=T_A+T_B=25-30=-5, \quad T_{CD}=T_{DE}=T_A+T_B+T_C =25-30+35=+30\ [\text{kN}\cdot\text{m}]$$
  2. Polar moments of inertia. $$J_{AB}=\frac{\pi(100)^4}{32}=9.817\times10^6\ \text{mm}^4, \quad J_{BC}=\frac{\pi(60)^4}{32}=1.272\times10^6\ \text{mm}^4$$ $$J_{CD}=\frac{\pi(120)^4}{32}=20.36\times10^6\ \text{mm}^4, \quad J_{DE}=\frac{\pi(120^4-60^4)}{32}=19.09\times10^6\ \text{mm}^4$$
  3. Part (a): shear stress in each segment, at its outer radius. $$\tau_{AB}=\frac{T_{AB}r_{AB}}{J_{AB}}=\frac{25\times10^6(50)}{9.817\times10^6} =\boxed{127.3\ \text{MPa}}\ \text{(governs)}$$ $$\tau_{BC}=117.9\ \text{MPa}, \qquad \tau_{CD}=88.4\ \text{MPa}, \qquad \tau_{DE}=94.3\ \text{MPa}$$ Segment AB governs at $\tau_{max}=127.3$ MPa ($<200$ MPa yield, OK). In every segment τ varies LINEARLY from zero at the shaft's centre to this maximum at the outer radius (for the hollow segment DE, from a non-zero value at the 30 mm inner radius up to the maximum at the 60 mm outer radius).
  4. Part (b): angle of twist, A relative to E. Sum $\phi_i=T_iL_i/(GJ_i)$ (signed, CW+) over all four segments (G = 25{,}000 MPa): $$\phi_{AB}=+2.918^\circ, \ \phi_{BC}=-2.702^\circ, \ \phi_{CD}=+1.351^\circ, \ \phi_{DE}=+2.882^\circ$$ $$\boxed{\phi_{A/E}=\Sigma\phi_i = +4.45^\circ}\ \text{(net clockwise, viewed from A)}$$
  5. Part (c): doubling all three torques. The shaft remains linear-elastic as long as no segment yields, so both τ and φ scale directly with T: every stress and the total twist would exactly DOUBLE (new $\tau_{max}=254.6$ MPa, new $\phi=8.90^\circ$). However $254.6\ \text{MPa} > 200\ \text{MPa}$ (yield), so segment AB (and possibly BC) would actually begin to YIELD; the true response would become elastic-plastic and the simple doubling relationship would no longer hold once yielding starts.

Final Results.

QuantityValue
TAB, TBC, TCD=TDE+25, −5, +30 kN·m
(a) τmax127.3 MPa, in segment AB
(b) φA/E4.45°, clockwise
(c) Loads doubledτ, φ would double if still elastic, but 254.6 MPa > 200 MPa yield → AB yields, no longer proportional
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